# Service difficulty reports: Boeing 727-77C

A list on [Boeing 727-77C](https://openairdocs.org/model/boeing-727-77c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 56 reports

- [SDR AUS20020240](https://openairdocs.org/sdr/AUS20020240.md): Balance Weight · corroded · Feb 15, 2002 · Boeing 72777C · Elevator, Tab Structure
  > (AUS) RH ELEVATOR TAB CENTRE BALANCE WEIGHT SPLIT OPEN DUE TO CORROSION.
- [SDR AUS20020241](https://openairdocs.org/sdr/AUS20020241.md): Panel · corroded · Feb 14, 2002 · Boeing 72777C · Horizontal Stabilizer, Plate/Skin
  > (AUS) HORIZONTAL STABILISER PANEL LOCATED ABOVE BAY THREE CORRODED IN AREA OF REAR AUXILIARY SPAR LH SIDE.
- [SDR AUS20020252](https://openairdocs.org/sdr/AUS20020252.md): Skin · corroded · Feb 6, 2002 · Boeing 72777C · Fuselage Main, Structure
  > (AUS) MAIN CARGO DOOR SUPPORT STRUCTURE TOP FORWARD CORNER CORRODED.CORROSION LOCATED AT ZONE 2-24, STN 48D, STRINGER 1LH TO STRINGER 3.
- [SDR AUS20020251](https://openairdocs.org/sdr/AUS20020251.md): Door · corroded · Feb 6, 2002 · Boeing 72777C · Cargo/Baggage Doors
  > (AUS) MAIN CARGO DOOR STRUCTURE LAP JOINT CORRODED AT STN 620.CORROSION IS LOCATED AT ZONE 2-48, STN 620 TO STN 623, STRINGER 9LH TO STRINGER 11.
- [SDR AUS20020250](https://openairdocs.org/sdr/AUS20020250.md): Door · corroded · Feb 6, 2002 · Boeing 72777C · Cargo/Baggage Doors
  > (AUS) MAIN CARGO DOOR STRUCTURE CORRODED AT THE LAP JOINT LOCATED ATSTN 620. CORROSION LOCATED AT ZONE 2-48, STN 620 TO STN 623,STRINGER 4LH TO STRINGER 5.
- [SDR AUS20020249](https://openairdocs.org/sdr/AUS20020249.md): Spar · corroded · Jan 30, 2002 · Boeing 72777C · Wing Spar
  > (AUS) LT REAR WING SPAR UPPER AND LOWER CHORDS CORRODED IN AREA LOCATED BEHIND THE VERTICAL STIFFENER. CORROSION LOCATED AT ZONE 6-72, WS 437 TO WS 438 LT.
- [SDR AUS20020248](https://openairdocs.org/sdr/AUS20020248.md): Structure · corroded · Jan 30, 2002 · Boeing 72777C · Wing Main, Frame Structure
  > (AUS) UPPER RT WING TOP CHORD CORRODED. CORROSION LOCATED AT ZONE 6-76, WS 351RT TO WS 355 RT.
- [SDR AUS20020246](https://openairdocs.org/sdr/AUS20020246.md): Support · corroded · Jan 30, 2002 · Boeing 72777C · Fuselage, Landing Gear Attach Fittings
  > (AUS) LH MAIN LANDING GEAR DOOR SEQUENCING STRIKER FRAME CORRODED.LOCATION OF CORROSION ZONE 1-35, STN 880, STRINGER 20LH, WL 152,BL70LH.
- [SDR AUS20020247](https://openairdocs.org/sdr/AUS20020247.md): Stiffener · corroded · Jan 29, 2002 · Boeing 72777C · Fuselage Miscellaneous Structure
  > (AUS) LT MAIN LANDING GEAR BAY STIFFENER CHORD CORRODED IN SEVERAL AREAS INCLUDING ATTACHMENT TO PRESSURE DECK. CORROSION LOCATED IN ZONE 1-35, STN 870, STRINGER 20 LT TO STRINGER 17, WL 208 TO WL184, BL 67 LT.
- [SDR AUS20020253](https://openairdocs.org/sdr/AUS20020253.md): Skin · corroded · Jan 27, 2002 · Boeing 72777C · Fuselage Main, Plate/Skin
  > (AUS) SKIN CORRODED IN AREA BELOW TOILET SERVICE DOOR. CORROSIONLOCATED AT ZONE 2-11, STN 350 TO STN 370, STRINGER 18RH.
- [SDR AUS20020245](https://openairdocs.org/sdr/AUS20020245.md): Frame · corroded · Jan 25, 2002 · Boeing 72777C · Fuselage, Landing Gear Attach Fittings
  > (AUS) RH MAIN LANDING GEAR WHEEL WELL DOOR SEQUENCING STRIKER FRAME CORRODED. FRAME LOCATED IN ZONE 1-36, STN 880, STRINGER 520RH,WL157, BL70RH.
- [SDR AUS20020244](https://openairdocs.org/sdr/AUS20020244.md): Plate · corroded · Jan 23, 2002 · Boeing 72777C · Fuselage, Door Hinge
  > (AUS) CARGO DOOR HINGE SUPPORT PLATE CORRODED. PLATE IS LOCATED IN ZONE 2-48, STN 520 TO STN 530, STRINGER 55LH.
- [SDR AUS20020243](https://openairdocs.org/sdr/AUS20020243.md): Track · corroded · Jan 22, 2002 · Boeing 72777C · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) CARGO TRACK CORRODED. TRACK IS LOCATED IN ZONE 1-13 SECTION 43, STN 540 TO STN 600 WL 156, BL16.
- [SDR AUS20020242](https://openairdocs.org/sdr/AUS20020242.md): Track · corroded · Jan 22, 2002 · Boeing 72777C · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) FORWARD CARGO TIEDOWN TRACK CORRODED.
- [SDR AUS20011198](https://openairdocs.org/sdr/AUS20011198.md): Hinge · failed · Nov 2, 2001 · Boeing 72777C · Leading Edge Devices
  > (AUS) NR 3 LEADING EDGE FLAP ACTUATOR HINGE FAILED.
- [SDR AUS20011040](https://openairdocs.org/sdr/AUS20011040.md): Housing · cracked · Sep 12, 2001 · Boeing 72777C · Landing Gear Door Actuator
  > (AUS) MAIN LANDING GEAR DOOR ACTUATOR LOWER BODY HOUSING CRACKED. LOSS OF HYDRAULIC FLUID.
- [SDR 2001F00178](https://openairdocs.org/sdr/2001F00178.md): Hinge Bracket · out of adj · Jul 4, 2001 · N526PC · Boeing 72777C · Landing Gear Doors
  > MAIN GEAR DOOR WILL NOT LOCK UP POSITION. GEAR INDICATED DOWN AND LOCKED WHEN CYCLED. PERFORMED ALL COMPANY PROCEDURES AND CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUSTED AND RESECURED FORWARD LEFT MAIN GEAR DOOR HINGE PLATE. LUBRICATED MAIN GEAR AN
- [SDR 20010601CW012](https://openairdocs.org/sdr/20010601CW012.md): Connector · loose · May 5, 2001 · N526PC · Boeing 72777C · Landing Gear Position and Warning
  > NO GEAR LIGHT WITH LANDING GEAR DOWN. EMERGENCY DECLARED. CORRECTION: RESECURED CANNON PLUG ON BACK OF LANDING GEAR LIGHT ASSEMBLY. LIGHTS OPERATE NORMAL.
- [SDR AU010334](https://openairdocs.org/sdr/AU010334.md): Actuator · faulty · Mar 15, 2001 · Boeing 72777C · Cargo/Baggage Doors
  > (AUS) MAIN CARGO DOOR REAR ACTUATOR EYE END BEARING MIGRATED RESULTING IN DISTORTION OF THE EYE END. MINOR DAMAGE TO RETRACTION ARM.
- [SDR AU000860](https://openairdocs.org/sdr/AU000860.md): Spar · corroded · Sep 2, 2000 · Boeing 72777C · Wing Spar
  > (AUS) REAR SPAR UPPER CHORD CORRODED AT UPPER SKIN INTERFACE INBOARD OF NR 4 SPOILER INBOARD HINGE. FOUND DURING CORROSION INSPECTION.
- [SDR AU000859](https://openairdocs.org/sdr/AU000859.md): Skin · corroded · Sep 2, 2000 · Boeing 72777C · Fuselage Main, Plate/Skin
  > (AUS) LOWER CENTRE LINE FUSELAGE SKIN CORRODED AT STN 360. FOUND DURING CORROSION INSPECTION.
- [SDR AU000861](https://openairdocs.org/sdr/AU000861.md): Spar Cap · corroded · Sep 1, 2000 · Boeing 72777C · Wing Spar
  > (AUS) REAR SPAR CAP CORRODED AT UPPER SKIN INTERFACE ADJACENT TOOUTBOARD FLAP OUTBOARD JACKSCREW GEARBOX. FOUND DURING CORROSIONINSPECTION.
- [SDR AU000858](https://openairdocs.org/sdr/AU000858.md): Angle · corroded · Sep 1, 2000 · Boeing 72777C · Fuselage Miscellaneous Structure
  > (AUS) BULKHEAD T' ANGLE LOCATED IN RT WHEEL WELL AT STN 950 CORRODED AT KEEL BEAM ATTACHMENT. FOUND DURING CORROSION INSPECTION.
- [SDR AU000857](https://openairdocs.org/sdr/AU000857.md): Fitting · corroded · Sep 1, 2000 · Boeing 72777C · Wing Miscellaneous Structure
  > (AUS) SPLICE FITTING LOCATED BETWEEN STN 870 FORGING AND HORIZONTAL BEAM LOCATED IN LT WHEEL WELL CORRODED. FOUND DURING CORROSIONINSPECTION.
- [SDR AU000856](https://openairdocs.org/sdr/AU000856.md): Web · corroded · Sep 1, 2000 · Boeing 72777C · Wing Miscellaneous Structure
  > (AUS) UPPER WEB LOCATED IN THE LT UPPER WHEEL WELL AT STN 870 BETWEEN WBL 0 AND WBL 24.75 CORRODED. FOUND DURING CORROSION INSPECTION.
- [SDR AU000855](https://openairdocs.org/sdr/AU000855.md): Keelbeam · corroded · Sep 1, 2000 · Boeing 72777C · Fuselage Main, Keel
  > (AUS) KEEL BEAM WEB CORRODED AT STN 950 LOCATED IN THE UPPER AFT CORNER OF THE LT WHEEL WELL. FOUND DURING CORROSION INSPECTION.
- [SDR AU000541](https://openairdocs.org/sdr/AU000541.md): Mount · failed · Jul 13, 2000 · Boeing 72777C · Drag Control System
  > (AUS) NR 2 SPOILER ACTUATOR MOUNT ASSEMBLY INBOARD LOWER MOUNT BOLT HOLE LUG CRACKED AND OUTBOARD LOWER MOUNT BOLT HOLE LUG BROKEN.INBOARD LOWER MOUNT BOLT SHEARED.
- [SDR 2000ZZZM172](https://openairdocs.org/sdr/2000ZZZM172.md): Element · out of adjust · Nov 30, 1999 · N526PC · Boeing 72777C · Overheat Detection
  > FLT 714 - CLE-IND - ON CLIMB-OUT, WITH ENGINE AND WING ANTI-ICE ON, NR 3 STRUT OVERHEAT LIGHT COMES ON. FOUND ENGINE 3 STRUT FIRE DETECTION LOOP ROUTED TO CLOSE TO DUCT, REPOSITIONED AND OPERATION CHECK GOOD ON GROUND. (M)
- [SDR 99ZZZM772](https://openairdocs.org/sdr/99ZZZM772.md): Overheat Element · out of adjusted · Oct 10, 1999 · N526PC · Boeing 72777C · Overheat Detection
  > FLT 711 - EWR-IND - NR 3 ENGINE STRUT OVERHEAT LIGHT FLICKERS WITH ENGINE AND WING ANTI-ICE ON. LIGHT COMES ON WITH TEMPERATURE GAUGE SHOWING BETWEEN 200 DEGREES CELSIUS, 225 DEGREES CELSIUS. TURNED OFF RIGHT WING ANTI-ICE AND THE NR 3 ENGINE STRUT LIGHT REM
- [SDR 99ZZZM738](https://openairdocs.org/sdr/99ZZZM738.md): Overheat Light · illuminated · Oct 9, 1999 · N526PC · Boeing 72777C · Overheat Detection
  > FLT 611 - IND-EWR - NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FIGHT WITH ENGINE AND WING ANTI-ICE ON. TURNED OFF RIGHT WING ANTI-ICE VALVE AND NR 3 ENGINE STRUT OVERHEAT LIGHT REMAINS OUT FOR REMAINDER OF FLIGHT. TROUBLESHOT WITH SUPPLIED AIR AND WITH
- [SDR 99ZZZM737](https://openairdocs.org/sdr/99ZZZM737.md): Fire Loop · out of position · Sep 29, 1999 · N526PC · Boeing 72777C · Fire Detection
  > FLT 710 - IND - NR 3 ENGINE FIRE DETECTOR CIRCUIT LIGHT ILLUMINATED. REPOSITIONED NR 3 ENGINE FIRE DETECTION LOOP. (M)
- [SDR 99ZZZM736](https://openairdocs.org/sdr/99ZZZM736.md): Fire Loop · reconfigured · Sep 14, 1999 · N526PC · Boeing 72777C · Fire Detection
  > FLT 712 - IND - NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT ON IN FLIGHT. RECONFIGURED LOOP, SYSTEM CHECKS NORMAL, NR 3 ENGINE FIRE DETECTION CIRCUIT. (M)
- [SDR 99ZZZM713](https://openairdocs.org/sdr/99ZZZM713.md): Fire Loop · out of position · Sep 11, 1999 · N526PC · Boeing 72777C · Fire Detection
  > FLT 607 - SFO, NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES IN FLIGHT. REPOSITIONED NR 3 FIRE LOOP, SECURED COWLING. (M)
- [SDR AU990778](https://openairdocs.org/sdr/AU990778.md): Skin · delaminated · Aug 7, 1999 · Boeing 72777C · Elevator, Plate/Skin
  > (AUS) LEFT ELEVATOR TRAILING EDGE INBOARD SKIN DELAMINATED FOR APPROXIMATELY 50.8 MM (2 INCHES).
- [SDR AU990736](https://openairdocs.org/sdr/AU990736.md): Wire · damaged · Jun 18, 1999 · Boeing 72777C · Electrical Power System Wiring
  > (AUS) SEVEN ELECTRICAL CABLES DAMAGED AT THE OUTER INSULATION JACKET. NO EVIDENCE OF EXPOSED CONDUCTORS.
- [SDR AU990774](https://openairdocs.org/sdr/AU990774.md): Skin · corroded · May 26, 1999 · Boeing 72777C · Elevator, Plate/Skin
  > (AUS) ELEVATOR SKIN CORRODED AT STN 40, STN 73, STN 84, STN 106 AND STN 166. RT STABILIZER UPPER SKIN ABOVE REAR SPAR CONTAINED FIVE AREAS OF REPAIR.
- [SDR AU990779](https://openairdocs.org/sdr/AU990779.md): Plate · corroded · Apr 21, 1999 · Boeing 72777C · Fuselage Main, Frame
  > (AUS) FRAME REINFORCEMENT PLATE LOCATED AT STN 227.8 AT THE COCKPIT SIDEWALL CORRODED.
- [SDR AU990773](https://openairdocs.org/sdr/AU990773.md): Skin · corroded · Apr 16, 1999 · Boeing 72777C · Fuselage Main, Plate/Skin
  > (AUS) INTERIOR SKIN CONTAINED CORROSION IN THE FOLLOWING AREAS: 1. BS 1192 - AREA OF CORROSION 25.4 MM BY 177.8 MM (1 INCH BY 7 INCH). 2. BS 1212 - AREA OF CORROSION 38.1 MM BY 101.6 MM (1.5 INCHES BY 4 INCHES). 3. BS 1232 - AREA OF CORROSION 38.1 MM BY
- [SDR AU990780](https://openairdocs.org/sdr/AU990780.md): Floorbeam · corroded · Apr 15, 1999 · Boeing 72777C · Fuselage Main, Floor Beam
  > (AUS) FUSELAGE FLOORBEAM LOCATED AT STN 344 LBL 2 CORRODED.
- [SDR AU990782](https://openairdocs.org/sdr/AU990782.md): Flange · corroded · Apr 14, 1999 · Boeing 72777C · Fuselage Miscellaneous Structure
  > (AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.
- [SDR AU990781](https://openairdocs.org/sdr/AU990781.md): Bracket · corroded · Apr 14, 1999 · Boeing 72777C · Fuselage Miscellaneous Structure
  > (AUS) MAIN CARGO BARRIER LOWER FITTING SUPPORT BRACKET LOCATED AT STN 375 RBL 39 CORRODED.
- [SDR AU990785](https://openairdocs.org/sdr/AU990785.md): Bulkhead · corroded · Apr 9, 1999 · Boeing 72777C · Fuselage Main, Bulkhead
  > (AUS) E/E COMPARTMENT BULKHEAD LOCATED AT STN BS 350.2, BL RBL 36 CORRODED. AREA OF CORROSION 1935.48 SQMM (3 SQUARE INCHES).
- [SDR AU990784](https://openairdocs.org/sdr/AU990784.md): Flange · corroded · Apr 9, 1999 · Boeing 72777C · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT STN 847 RBL 63.
- [SDR AU990783](https://openairdocs.org/sdr/AU990783.md): Flange · corroded · Apr 9, 1999 · Boeing 72777C · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.
- [SDR AU990772](https://openairdocs.org/sdr/AU990772.md): Stiffener · corroded · Apr 8, 1999 · Boeing 72777C · Wing Miscellaneous Structure
  > (AUS) RIGHT WING FRONT SPAR STIFFENER CONTAINED LEVEL 2 CORROSION.
- [SDR AU990777](https://openairdocs.org/sdr/AU990777.md): Beam · corroded · Apr 7, 1999 · Boeing 72777C · Horizontal Stabilizer Structure
  > (AUS) RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED FOR APPROXIMATELY 127 MM (5 INCHES) BETWEEN STN 200 AND STN 209.
- [SDR AU990776](https://openairdocs.org/sdr/AU990776.md): Spar · corroded · Apr 7, 1999 · Boeing 72777C · Horizontal Stabilizer, Spar/Rib
  > (AUS) RIGHT STABILIZER REAR SPAR UPPER CHORD BULGED AND CORRODED FOR APPROXIMATELY 177.8 MM (7 INCHES) BETWEEN STN 176 AND STN 186.
- [SDR AU990775](https://openairdocs.org/sdr/AU990775.md): Skin · corroded · Apr 7, 1999 · Boeing 72777C · Elevator, Plate/Skin
  > (AUS) LET ELEVATOR LOWER SKIN BULGED AND CORRODED BETWEEN SEVEN RIVETS AT STN 159 TRAILING EDGE.
- [SDR AU990358](https://openairdocs.org/sdr/AU990358.md): Harness · failed · Feb 24, 1999 · Boeing 72777C · DC Power Distribution System
  > (AUS) BURNED WIRE BUNDLE LOCATED IN THE FORWARD E/E COMPARTMENT AT STN 296-312 IN THE RT SIDE UNDER THE TOILET SERVICE DUCT. A TOTAL OF 68 WIRES REPLACED.
- [SDR 99ZZZM139](https://openairdocs.org/sdr/99ZZZM139.md): Engine · damaged · Dec 8, 1998 · N526PC · Boeing 72777C · Engine (Turbine/Turboprop)
  > FLT 614 - BUF - NR 3 ENGINE HAS FOREIGN OBJECT DAMAGE. REMOVED AND REPLACED NR 3 ENGINE. DUE TO BAD WEATHER AIRCRAFT COULD NOT FERRY TO IND UNTIL 1/17/99, WHERE MAINTENANCE WAS PERFORMED. (M)

Next page: https://openairdocs.org/model/boeing-727-77c/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '72777C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-77c/reports

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